Laser-Supported Directed-Energy "Air Spike" in Hypersonic Flow von Minucci, M. A. S, Toro, P. G. P, Oliveira, A. C, Ramos, A. G, Chanes, J. B, Pereira, A. L, Nagamatsu, H. T, Myrabo, L. N

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Investigation of a Laser-Supported Directed-Energy "Air Spike" in Hypersonic Flow von Minucci, M. A. S, Toro, P. G. P, Chanes, J. B, Ramos, A. G, Pereira, A. L, Nagamatsu, H. T, Myrabo, L. N

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Experimental and Computational Investigation of Drag Reduction by Electric-Arc Airspikes at Mach 10 von Hartley, C S, Portwood, T W, Filippelli, M V, Myrabo, L N, Nagamatsu, H T, Shneider, M N, Razier, Y P

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Hypersonic shock-tunnel testing at an equilibrium interface condition of 4100 K von Minucci, M. A. S, Nagamatsu, H. T

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Investigation of ramped air arcs near current zero in dual-flow nozzle system von Serbetci, I., Nagamatsu, H.T.

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Investigation of a two-dimensional scramjet inlet, freestream M = 8-18 and T0 = 4100 K von Minucci, M. A. S, Nagamatsu, H. T

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Numerical study of low-current steady arcs von Kim, S. C, Nagamatsu, H. T

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Schlieren Visualization Technique Applied to the Study of Laser-Induced Breakdown in Low Density Hypersonic Flow von Oliveira, A C, Minucci, M A S, Toro, P G P, Chanes Jr, J B, Salvador, I I, Myrabo, L N, Nagamatsu, H T

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Development of a New Hypersonic Shock Tunnel Facility to Investigate Electromagnetic Energy Addition for Flow Control and Basic Supersonic Combustion von Toro, P G P, Minucci, M A S, Chaves Jr, J B, Pereira, A L, Nagamatsu, H T

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Experimental study of a two-dimensional scramjet inset, M(freestream) = 10.1-25.1 von Minucci, M. A. S, Nagamatsu, H. T

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Experimental investigation of an axisymmetric hypersonic scramjet inlet for laser propulsion von Jones, R. A, Myrabo, L. N, Nagamatsu, H. T, Minucci, M. A. S

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Combustion shock tunnel and interface compression to increase reservoir pressure and enthalpy von Minucci, M. A. S, Nagamatsu, H. T, Myrabo, L. N

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Heat transfer in the stagnation region of the junction of a circular cylinder perpendicular to a flat plate von Hinckel, Jose N., Nagamatsu, H.T.

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Experimental and theoretical study of a direct-current arc in an orifice nozzle flow von Whang, H. C, Nagamatsu, H. T

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Heat transfer and transition mechanism on a shock-tube wall von Dillon, R. E, Nagamatsu, H. T

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Low Reynolds number aerodynamic characteristics of low-drag NACA 63-208 airfoil von Nagamatsu, H. T, Cuche, D. E

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Theoretical and Experimental Investigations of the Flow Field for Asymmetric Dual-Flow Interrupter Nozzles von Nagamatsu, H. T., Whang, H. C.

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Nature of convection-stabilized dc arcs in dual-flow nozzle geometry. I - The cold flow field and dc arc characteristics. II - Optical diagnostics and theory von Serbetci, Ilter, Nagamatsu, H. T.

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Nature of convection-stabilized DC arcs in dual-flow nozzle geometry. II. Optical diagnostics and theory von Serbetci, I., Nagamatsu, H.T.

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Numerical Investigation of Vibrational Nonequilibrium Effects in Hydrogen - Oxygen Rocket Engines von Jones, Richard A, Myrabo, Leik N, Nagamatsu, Henry T

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